A composite structure includes a base and an auxiliary portion of dissimilar materials. The auxiliary portion is shaped by stamping. As the auxiliary portion is stamped, it interlocks with the base, and at the same time forming a desired structured feature on the auxiliary portion, such as a structured reflective surface, an alignment feature, etc. With this approach, relatively less critical structured features can be shaped on the bulk of the base with less effort to maintain a relatively larger tolerance, while the relatively more critical structured features on the auxiliary portion are more precisely shaped with further considerations to define dimensions, geometries and/or finishes at relatively smaller tolerances. The auxiliary portion may include a composite structure of two dissimilar materials associated with different properties for stamping different structured features.
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1. A method of forming a composite structure having structured features defined thereon to define an optical path in connection with optical transmissions, comprising:
providing a base comprising a body of a first material defined between a top surface and a bottom surface, wherein the base is provided with a top opening at the top surface, a bottom opening at the bottom surface, and a through hole extending through the body from the top opening at the top surface to the bottom opening at the bottom surface of the body;
positioning a second material in the through hole provided in the base, wherein the second material is dissimilar to the first material; and
stamping the second material to structurally couple the second material to the base and to define a first structured feature on the second material, thereby forming the composite structure comprising the base of the first material and an auxiliary portion from the second material with the first structured feature defined thereon, and
wherein the first structured feature defines an optical path in connection with optical transmissions.
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This application is a continuation of U.S. patent application Ser. No. 14/714,211 filed on May 15, 2015, which (1) claims the priority of U.S. Provisional Patent Application No. 61/994,094 filed on May 15, 2014, and (2) is a continuation-in-part of U.S. patent application Ser. No. 14/695,008 filed on Apr. 23, 2015, which is a continuation-in-part of U.S. patent application Ser. No. 13/861,273 filed on Apr. 11, 2013, which (a) claims the priority of U.S. Provisional Patent Application No. 61/623,027 filed on Apr. 11, 2012; (b) claims the priority of U.S. Provisional Patent Application No. 61/699,125 filed on Sep. 10, 2012; and (c) is a continuation-in-part of U.S. patent application Ser. No. 13/786,448 filed on Mar. 5, 2013, which claims the priority of U.S. Provisional Patent Application No. 61/606,885 filed on Mar. 5, 2012. These applications are fully incorporated by reference as if fully set forth herein. All publications noted below are fully incorporated by reference as if fully set forth herein.
The present invention relates to precision stamping, in particular precision stamping to produce devices for use in connection with optical signal transmissions, and more particularly to precision stamping to produce devices for routing optical data signals.
The Assignee of the present invention, nanoPrecision Products, Inc., developed various proprietary devices used in connection with optical data transmission. For example, US2013/0322818A1 discloses an optical coupling device having a stamped structured surface for routing optical data signals, in particular an optical coupling device for routing optical signals, including a base; a structured surface defined on the base, wherein the structured surface has a surface profile that reshapes and/or reflect an incident light; and an alignment structure defined on the base, configured with a surface feature to facilitate positioning an optical component on the base in optical alignment with the structured surface to allow light to be transmitted along a defined path between the structured surface and the optical component, wherein the structured surface and the alignment structure are integrally defined on the base by stamping a malleable material of the base.
US2013/0294732A1 further discloses a hermetic optical fiber alignment assembly having an integrated optical element, in particular a hermetic optical fiber alignment assembly including a ferrule portion having a plurality of grooves receiving the end sections of optical fibers, wherein the grooves define the location and orientation of the end sections with respect to the ferrule portion. The assembly includes an integrated optical element for coupling the input/output of an optical fiber to optoelectronic devices in an optoelectronic module. The optical element can be in the form of a structured reflective surface. The end of the optical fiber is at a defined distance to and aligned with the structured reflective surface. The structured reflective surfaces and the fiber alignment grooves can be formed by stamping.
U.S. patent application Ser. No. 14/695,008 further discloses an optical coupling device for routing optical signals for use in an optical communications module, in particular an optical coupling device in which defined on a base are a structured surface having a surface profile that reshapes and/or reflect an incident light, and an alignment structure defined on the base, configured with a surface feature to facilitate positioning an optical component on the base in optical alignment with the structured surface to allow light to be transmitted along a defined path between the structured surface and the optical component. The structured surface and the alignment structure are integrally defined on the base by stamping a malleable material of the base. The alignment structure facilitates passive alignment of the optical component on the base in optical alignment with the structured surface to allow light to be transmitted along a defined path between the structured surface and the optical component. The structured surface has a reflective surface profile, which reflects and/or reshape incident light.
U.S. Pat. No. 7,343,770 discloses a novel precision stamping system for manufacturing small tolerance parts. Such inventive stamping system can be implemented in various stamping processes to produce the devices disclosed in the above-noted patent publications. These stamping processes involve stamping a bulk material (e.g., a metal blank), to form the final surface features at tight (i.e., small) tolerances, including the reflective surfaces having a desired geometry in precise alignment with the other defined surface features.
Heretofore, the bulk material that is subjected to stamping is a homogenous material (e.g., a strip of metal, such as Kovar, aluminum, etc.) The stamping process produces structural features out of the single homogeneous material. Thus, different features would share the properties of the material, which may not be optimized for one or more features. For example, a material that has a property suitable for stamping an alignment feature may not possess a property that is suitable for stamping a reflective surface feature having the best light reflective efficiency to reduce optical signal losses.
What is needed is an improved stamping process to produce devices with improved structural characteristics, functionalities, performances, reliability and manufacturability, at reduced costs.
The present invention further improves over the earlier stamping processes, by providing a composite structure that is precision stamped to form structured features (e.g., micro features), and more particularly devices having such structured features for use in connection with optical signal transmissions (including optical transmissions for micro electro-mechanical systems (MEMS) such as sensors).
According to the present invention, the composite structure comprises at least two dissimilar materials having one or more dissimilar properties, including without limitations chemical, physical, thermal, electrical, structural etc. properties, which may be optimized to enhance the functionalities of the structured features to be defined by these dissimilar materials. In particular, the composite structure comprises a body having a base comprising a base material and at least an auxiliary portion comprising at least a dissimilar auxiliary material that is paired or complementary to the base material. The auxiliary portion is coupled to the base. At least the auxiliary material of the auxiliary portion is shaped by stamping to form at least one structured feature that takes advantage of the properties of the auxiliary material (e.g., a light reflective surface feature and/or an alignment feature for a light guide or a light source/receiver). The base may also be shaped to define different structured feature(s) that take advantage of the properties of the base material.
In the composite structure, the dissimilar materials are distinctly present at different portions of the composite structure (i.e., at the base and auxiliary portion), thus exhibiting different properties of the respective dissimilar materials at different portions of the composite structure. Accordingly, in the context of the present invention, the auxiliary material is structurally coupled or attached to the base material to define a composite structure having the different materials remaining substantially distinct in bulk at different parts of the composite structure (ignoring any possible slight compounding/alloying present at a molecular level near the surfaces at the interface of the two different materials), in contrast to a structure in which, in bulk, constitutes a matrix based composite, a compound, an alloy and/or a solid solution of two of more dissimilar materials.
The base may provide a bulk support body on which the auxiliary portion is coupled. At least the auxiliary portion is stamped to define one or more structured features. In addition or in the alternate, the base may include structured features pre-defined thereon (e.g., by stamping) prior to coupling/stamping the auxiliary portion. In addition, a final stamping step may be undertaken with respect to the auxiliary material and/or the base material to obtain the desired finish, geometry and dimension of the structured feature at the auxiliary portion and/or the base.
In one embodiment, at least a dissimilar portion having an auxiliary material is coated onto at least part of the base. In another embodiment, the dissimilar portion may be attached to the base by other means (e.g., bonding, welding, riveting, etc.)
In another embodiment, at least one dissimilar auxiliary portion is coupled to the base by stamping. The auxiliary material may be fused to the base material under pressure from stamping the dissimilar material onto the base material; this is possible when the base portion and auxiliary portion have similar chemical composition (e.g. two aluminum alloys). Alternatively, the auxiliary material is structurally interlocked to the base material by stamping. In one embodiment, the auxiliary material is configured in the form of an insert, which is disposed in an opening in the base. The insert is stamped, creating an interlocking structure (e.g., a plug or a rivet-like interlocking structure) with respect to the base, and at the same time forming a desired structured feature on the insert.
The auxiliary material is chosen to be malleable for shaping by stamping. The base material may also be chosen to be malleable for shaping by stamping. In one embodiment, the auxiliary material is chosen to be relatively more malleable/ductile than the base material, to obtain the desired geometries, dimensions and/or finishes of critical features (e.g., a high optical reflective surface) at the auxiliary portion.
In one embodiment of the present invention, the base may be shaped (e.g., by stamping) to define structured feature(s) having relatively less critical dimensions, geometries and finishes based on relatively larger tolerances, and the auxiliary portion is shaped to define structured feature(s) having relatively more critical dimensions, geometries and/or finishes based on relatively smaller tolerances. With this approach, relatively less critical structured features can be shaped on the bulk of the base with less effort to maintain a relatively larger tolerance, while the relatively more critical structured features on the auxiliary portion are more precisely shaped with further considerations to define dimensions, geometries and/or finishes at relatively smaller tolerances.
In a further embodiment, the auxiliary portion (e.g., in the form of a plug or rivet) comprises a composite structure comprising at least two dissimilar auxiliary materials (e.g., a bi-metallic material) associated with different properties for stamping different structured features.
In one embodiment, an optical bench and/or an optical coupling device can be formed by stamping to form a composite structure as above. The auxiliary portion is shaped to define a structured reflective surface, and further structured features for aligning the end portions of the optical fibers with respect to the structured reflective surfaces. The auxiliary portion may comprise a first type of auxiliary material for stamping the structured reflective surface and a dissimilar second type of auxiliary material for stamping the structured features for alignment. The base is shaped to define relatively less dimensionally critical structured features, such as grooves for retaining optical fibers.
The composite structure of the present invention may include the following: (a) a metal auxiliary material and a metal base material; (b) a metal auxiliary material and a non-metal base material; and (c) a non-metal auxiliary material and a metal base material.
The present invention can be implemented to precisely form micro structured features in various devices, such as those disclosed in the patent documents assigned to nanoPrecision Products, Inc. which have been discussed in the Background section herein. The present invention can be implemented to produce optical subassemblies and stamped optical benches having structured features that achieve or exceed the functionalities of silicon optical benches discussed, for example, in US2003/223131A1; U.S. Pat. Nos. 6,869,231; 8,103,140; and 8,168,939.
For a fuller understanding of the nature and advantages of the invention, as well as the preferred mode of use, reference should be made to the following detailed description read in conjunction with the accompanying drawings. In the following drawings, like reference numerals designate like or similar parts throughout the drawings.
This invention is described below in reference to various embodiments with reference to the figures. While this invention is described in terms of the best mode for achieving this invention's objectives, it will be appreciated by those skilled in the art that variations may be accomplished in view of these teachings without deviating from the spirit or scope of the invention.
The present invention further improves over the earlier stamping processes, by providing a composite structure that is precision stamped to form structured features, and more particularly devices having such structured features for use in connection with optical signal transmissions.
The concept of the present invention will be discussed with reference to an example of an optical coupling device for use to physically and optically coupling an input/output end of an optical component (e.g., an optical fiber) for routing optical signals. The present invention may be applied to form structures and parts used in other fields.
In the example discussed below, the coupling device is implemented with a stamped reflective surface for routing/redirecting optical signals from/to an external transmitter (Tx)/receiver (Rx) to/from an optical fiber. The structures of the optical coupling devices discussed below redirect light in similar fashion as the structures disclosed in connection with the optical coupling device in, for example, US2013/0294732A1. The present invention however adopts a different approach to defining the structured features associated with redirecting light (which may include structured reflective surfaces and associated alignment features), by implementing the inventive composite structures and associated stamping processes to define the structured features in the devices.
The auxiliary portion 14 is shown more clearly in
As more clearly shown in
It is noted that the auxiliary portion 14 shown in
In accordance with the present invention, the optical coupling device 10 is represented by a composite structure that comprises at least two dissimilar materials having one or more dissimilar properties, including without limitations chemical, physical, thermal, electrical, structural etc. properties, which may be optimized to enhance the functionalities of the structured features to be defined by these dissimilar materials. In particular, the composite structure of the body of the optical coupling device 10 has a base 16 comprising a base material and an auxiliary portion 14 comprising at least a dissimilar auxiliary material that is paired or complementary to the base material. The auxiliary portion 14 is coupled/attached to the base 16 to form the composite structure. At least the auxiliary material of the auxiliary portion 14 is shaped by stamping to form at least one structured feature (e.g., a structured reflective surface 12) that takes advantage of the properties of the auxiliary material and/or an alignment feature (e.g., grooves) for a light guide (e.g., an optical fiber 20). The base 16 may also be shaped to define additional structured feature(s) (e.g., grooves 17 for retaining optical fibers 20) that separately take advantage of the different properties of the base material.
In the composite structure, the dissimilar materials are distinctly present at different portions of the composite structure (i.e., at the base and auxiliary portion), thus exhibiting different properties of the respective dissimilar materials at different portions of the composite structure. Accordingly, in the context of the present invention, the auxiliary material is structurally coupled or attached to the base material to define a composite structure having the different materials remaining substantially distinct in bulk at different parts of the composite structure, in contrast to a structure in which, in bulk, constitutes a matrix based composite, a compound, an alloy and/or a solid solution of two of more dissimilar materials.
The base 16 thus provide a bulk support body on which the auxiliary portion 14 is coupled. In accordance with the present invention, at least the auxiliary portion 14 is stamped to define one or more structured features. In addition or in the alternate, the base 16 may include structured features pre-defined thereon (e.g., grooves 17 by stamping) prior to coupling/stamping the auxiliary portion 14. In addition, a final stamping step may be undertaken with respect to the auxiliary material and/or the base material to obtain the final desired finish, geometry and dimension of the structured feature at the auxiliary portion and/or the base. The base 16 may be shaped (e.g., by stamping) to define structured feature(s) having relatively less critical dimensions, geometries and finishes based on relatively larger tolerances, and the auxiliary portion 14 is shaped to define structured feature(s) having relatively more critical dimensions, geometries and/or finishes based on relatively smaller tolerances (e.g., a tolerance less than 1000 nm for purpose of optical data signal transmission). With this approach, relatively less critical structured features can be shaped on the bulk of the base 16 with less effort to maintain a relatively larger tolerance, while the relatively more critical structured features on the auxiliary portion 14 are more precisely shaped with further considerations to define dimensions, geometries and/or finishes at relatively smaller tolerances.
Essentially, for the optical coupling device 10, the base 16 and the auxiliary portion 14 together form a composite structure defining an optical bench 11 for aligning the optical fibers 20 with respect to the structured reflective surfaces 12, with the auxiliary portion 14 defining the structured reflective surface 12 and the alignment grooves 25 with relatively more critical geometries, dimensions and/or finishes desired for aligning the optical fiber end sections 21 with respect to the structured reflective surfaces 12, and the base 16 includes a structure defining open grooves 17 with relatively less critical geometries, dimensions and/or finishes for retaining the bulk sections of the bare optical fibers 20 without optical alignment concern. By including the grooves 25 on the same, single structure that also defines the structured reflective surfaces 12, the alignment of the end sections 21 of the optical fibers 20 to the structured reflective surfaces 12 can be more precisely achieved with relatively smaller tolerances by a single final stamping to simultaneous define the final structure on a single part, as compared to trying to achieve similar alignment based on features defined on separate parts or structures. By forming the structure reflective surfaces 12 and the optical fiber alignment structure/grooves 25 simultaneously in a same, single final stamping operation, dimensional relationship of all features/components requiring (or play a role in providing) alignment on the same work piece/part can be maintained in the final stamping step. Further, the material for the auxiliary portion 14 may be chosen to possess a high reflective efficiency (e.g., pure Aluminum) that is desirable for the structured reflective surface 12 having high optical reflectance, and the dissimilar material for the base 16 may be chosen to possess properties desirable for the base 16, such as high rigidity, low coefficient of thermal expansion, etc.
The overall functional structures of the optical bench 11 (and bench 11′ in
In one aspect of the present invention, the material of the auxiliary portion 14 is coupled to the dissimilar material of the base 14 at the same time the structured features on the auxiliary portion 14 are formed by stamping. In one embodiment, the auxiliary material is structurally interlocked to the base material by stamping, e.g., in a rivet-like manner as in the embodiments of
Referring to
For sake of simplicity, a preformed base 16 is positioned on the die 43, below the punch guide 42, with the through-hole 15 aligned with the tip of the punch 41. The spacer 19 is supported between the flat die 46 and the base 16 and may be joined to the base by a previous joining process like welding or gluing. The insert 34 is placed in the through-hole 15 in the base 16.
Referring to
Instead of a punching operation with a single strike of the punch 41, it is conceivable that multiple strikes may be implemented to progressive pre-form certain features on the auxiliary portion 14, with a final strike to simultaneously define the final dimensions, geometries and/or finishes of the various structured features on the auxiliary portion 14. By forming the structure reflective surfaces 12 and the optical fiber alignment structure/grooves 25 simultaneously in a same, single final stamping operation, dimensional relationship of all features/components requiring (or play a role in) alignment on the same work piece/part can be maintained in the final stamping step.
The formation of impressions, i.e., the structured features, on the surface of the auxiliary portion 14 involves a process generally known as “coining”. According to one embodiment of the present invention, the structured features of the auxiliary portion 14 may be formed by precision stamping a ductile or malleable material, preferably metal, such as pure Aluminum. Based on prior experimental results, it has been found that stamped structured reflective surfaces can achieve a peak-to-valley form error of less than 1 μm over a 1 mm diameter area. Surface roughness (Ra) based on scanning white light interferometry is on the order of 8 nm or better. The compression of the malleable material between the punch and die generates high contact pressure for a high reflective, mirror-quality surface.
A precision stamping process and apparatus has been disclosed in U.S. Pat. No. 7,343,770, which was commonly assigned to the assignee of the present invention. This patent is fully incorporated by reference as if fully set forth herein. The process and stamping system disclosed therein may be adapted to precision stamp the features of the optical bench 11 in the coupling device 10 of the present invention (including the structured features of the auxiliary portion 14 and the base 16 disclosed herein), which includes a composite structure as discussed above. The stamping process and system can produce parts with a tolerance of at least 1000 nm (i.e., a tolerance of 1000 nm or less/better). This system may be implemented to undertake various operations for stamping, such as forging, blanking, punching, coining, compression, bending, extruding, perforating, notching, etc. The above disclosed open structure of the coupling device having the structured reflective surface and the fiber retention structure lends itself to mass production processes such as stamping, which are low cost, high throughput processes. In the discussions throughout herein, various details of stamping systems and processes not essential to an understanding of the inventive concept have been omitted.
In operation, the spring-loaded retainer 54 is retracted to place the work piece/base 16 and insert 34 under the punch 41. The height of the flat die 46 is adjusted to support the spacer 19 at the desired location, by turning the spring plunger to move the wedge 56 horizontally. After stamping operation, the spring-loaded retainer 54 is retracted to release the stamped piece (i.e., base 16 with auxiliary portion 16 coupled thereto).
The stamping tool 50 may be incorporated in a stamping system that may include a progressive die, which provide an effective way to convert raw coil stock material into a finished product with minimal handling. The part material feeds one progression for each press cycle. As material feeds from station to station in the die, it progressively works into a complete part.
The strip 60 has a series of indexing holes 61 formed along a spine 62 of the strip 60. The strip 60 is fed through a series of stamping stations/dies, subject to precision stamping operations to form the desired features of the base 16. The indexing holes 61 are used for indexing the strip 60 as it is fed through the stamping stations. The entire strip 60 may be progressively fed through a first stamping station before the entire strip 60 is progressively fed through a second stamping station, and so forth. Alternatively, the strip 60 may be fed continuously through a series of progressive stamping stations (or a progressive die). The features on the base 16 in the optical bench 11 may be progressively formed via a sequence of stamping operations, with the final geometry of the features being defined by a single stamping operation within the sequence, to simultaneously define the final geometries, dimensions and/or finishes of the surface features of the base 16.
As earlier noted in connection with the earlier embodiments, the precision stamping process and apparatus as disclosed in U.S. Pat. No. 7,343,770 (which was commonly assigned to the assignee of the present invention) could be adopted to stamp strip 60 to form the features of the base 16.
As shown in
Arrow A represents the direction of feed of the strip 60. Section 64g represents a “finished” stamped section at the end of the stamping cycles, at which the features of the base 16 have been finally formed by stamping. Given the direction of feed (arrow A). Section 64a represents the start of the stamping cycles. As shown in
Specifically at section 64a, the outside boundary of the base is shaped (e.g., by a blanking operation). At sections 64b to 64c, surface features are progressive formed (e.g., the spacer 19, and the pocket 32 are formed by a forging operation). At section 64d, through-holes 15 and 31 are formed (e.g., by a punching operation). Grooves 17 are rough formed at section 64e (e.g., by a coining operation). At section 64f, the planar surfaces 63 about the grooves are flattened (e.g., by a compression operation). At section 64g, the grooves 17 are finally formed with precision. The sections 64e to 64g are designed to compensate for springback from stamping the relatively hard base material (e.g., Kovar). This completes the cycle for forming the structured features on the base 16. The base 16 is singulated by cutting along dotted lines 65) from the spine 62 in strip 60. The base 16 may be subject to further processing (e.g., surface finishing and/or coating, such as gold plating to improve anti-corrosion, etc.)
The singulated base 16 is turned upside down, and subject to stamping the metal insert 34 using the stamping tool 50 in
The above-described embodiment is illustrative of how a basic combination of features and components defined on an optical bench can be formed by stamping operations on a single part having a composite structure, to achieve a defined optical path 100 with optical alignment at tight (i.e., small) tolerances. Other configurations achieving different optical paths may be configured, such as re-configuring prior art silicon optical benches with stamped optical benches having similar defined optical paths. A stamped optical bench could have similar overall size and configuration, and similar footprint, compared to a corresponding silicon optical bench. The stamped optical bench would be backward compatible to replace a silicon optical bench. It is conceivable that stamped optical benches could be configured to have a smaller footprint and overall size than silicon optical benches.
The above described structured features at the surface of the auxiliary portion 14 are integrally stamped from the same stock material (i.e., insert 34). Matching punches and dies having appropriate features defined thereon may be applied in a series of stamping operations to obtain the desired geometries of the above-described features of the base 16 and auxiliary portion 14. Preferably, at least the features critical to precise optical alignment are subject to a final stamping operation, by which such features are finally defined simultaneously on the same (e.g., monolithic or unitary), single auxiliary portion 14. For the illustrated embodiments, this would include at least the structured reflective surface 12, the shoulder 5 and the alignment grooves 25. These structured features may be individually preformed during a sequence of stamping operations, but they are subject to a final stamping operation using a die having a surface profile 45 that integrally and/or simultaneously defines the final geometry of the combination of these features in relationship to each other on the same (monolithic or unitary) auxiliary portion 12. By forming the structure reflective surfaces 12 and the optical fiber alignment structure/grooves 25 simultaneously in a same, single final stamping operation, dimensional relationship of all critical features/components requiring (or play a role in providing) alignment on the same work piece/part can be maintained in the final stamping step. Accordingly, optical fibers 20, with their ends 21 retained in the alignment grooves 5, have end faces that are positioned in a precise predetermined relationship to the structured reflective surface 12, thus conforming to a desired optical path 100 at least between the optical fibers 20 and the structured reflective surfaces 12 (e.g., optical path 100 shown in
In accordance with another embodiment, instead of creating an interlocking rivet-like structure between the auxiliary portion 14 and the base 16 in the above-described embodiments, the base 16 and the spacer 19 are not provided with chamfers 26 and 27, and under stamping operation the insert 34 simply forms a tight mechanical fit in the through-hole 15 in the base 16.
In a further embodiment, the auxiliary material may be fused to the base material under pressure from stamping the dissimilar material onto the base material; this can be accomplished when the base and auxiliary portions are made of chemically similar metals (e.g. two aluminum alloys). For example, an auxiliary portion may be in the form of a layer of metal (e.g., pure Aluminum), which is stamped to form structured features and at the same time fusing to an underlying base material (e.g., Aluminum 6061 alloy), to form a composite structure.
In a further embodiment, an auxiliary portion in the form of a coating (e.g., gold plating) may be pre-formed on a base material, prior to stamping the coating to form structured features on the surface of the coating.
In the above described embodiments, the auxiliary material is chosen to be malleable for shaping by stamping operations. The base material may also be chosen to be malleable for shaping by stamping. In one embodiment, the auxiliary material (e.g., pure Aluminum) is chosen to be relatively softer, and more malleable/ductile than the base material (e.g., Kovar), to obtain the desired geometries, dimensions and/or finishes of critical features (e.g., a light reflective surface) at the auxiliary portion. The harder base material (e.g., Kovar) is chosen to form structures that require the integrity of a harder material, but stamping the harder base material would require larger forces and result in more springback, requiring multiple hits of the stamping punch to obtain the desire shape. In contrast, the relatively softer auxiliary material chosen for stamping the auxiliary portion requires less stamping forces and results in less springback, requiring relatively fewer hits (e.g., just one hit) of the punch to obtain the stamped part. Hence micro features can be stamped with very small tolerances. The harder base material also functions as part of the die, which partially shapes the auxiliary portion 14 during stamping operation.
In a further embodiment, the auxiliary portion (e.g., in the form of a slug or rivet) comprises a further composite structure comprising at least two dissimilar auxiliary materials (e.g., a bi-metallic material) associated with different properties for stamping different structured features.
Upon stamping, as shown in
In one embodiment, the material 170 could be an Aluminum alloy and the material 171 could be pure Aluminum. Aluminum alloy is a relatively harder material compared to pure Aluminum, which therefore result in a structure that possesses better structural integrity for aligning the optic fiber 20. Pure Aluminum, on the other hand, is chosen for its high optical reflectance. The material of the base 116 could be Kovar, selected for its strength, hardness, low coefficient of thermal expansion and glass matching characteristics for a glass sealant to achieve a hermetic seal.
Accordingly, in the embodiment of
While the foregoing embodiments are described in connection with composite structures having dissimilar metal materials, it is possible to form composite structure in accordance with the present invention to include the following: (a) a metal auxiliary material and a metal base material; (b) a metal auxiliary material and a non-metal base material; and (c) a non-metal auxiliary material and a metal base material. For example, the base may be made of a ceramic material, and the auxiliary portion made of a metal. The auxiliary portion can be stamped and pressed from a relatively soft and ductile metal insert inserted into the ceramic base. The ductile insert in the brittle ceramic body can be stamped and formed to obtain precise, detail surface features, including reflective optics. Thus reflective optics can be easily achieved in a ceramic substrate. Alternatively, an over molded polymer on a base may be stamped to form desired surface features.
In another embodiment, the dissimilar auxiliary portion may be attached to the base by other means (e.g., bonding, welding, riveting, etc.), prior to subjecting the auxiliary portion to stamping operation(s).
While the above embodiments are discussed in connection with optical fibers as optical components, optical benches having a composited structure may be structured to support and optically align other types of optical components, such as lenses, optical transmitters (Tx), optical receivers (Rx), optical transceivers (Tx/Rx), etc.
The present invention can be implemented to precisely form structured features in various devices, such as those disclosed in the patent documents assigned to nanoPrecision Products, Inc. which have been discussed in the Background section herein. The present invention can be implemented to produce optical subassemblies and stamped optical benches having structured features that achieve or exceed the functionalities of prior art silicon optical benches, such as those discussed in US2003/223131A1; U.S. Pat. Nos. 6,869,231; 8,103,140; and 8,168,939.
While the invention has been particularly shown and described with reference to the preferred embodiments, it will be understood by those skilled in the art that various changes in form and detail may be made without departing from the spirit, scope, and teaching of the invention. Accordingly, the disclosed invention is to be considered merely as illustrative and limited in scope only as specified in the appended claims.
Zhao, Yongsheng, Vallance, Robert Ryan, Mengesha, Tewodros, Dannenberg, Rand D., Barnoski, Michael K., Li, Shuhe, Gean, Matthew
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Sep 15 2015 | ZHAO, YONGSHENG | NANOPRECISION PRODUCTS, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 047558 | /0393 | |
Sep 15 2015 | BARNOSKI, MICHAEL K | NANOPRECISION PRODUCTS, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 047558 | /0393 | |
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